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<html><head>
<meta http-equiv="Content-Type" content="text/html; charset=UTF-8">
<title>Simulink Default Report</title><meta name="generator" content="DocBook XSL Stylesheets V1.75.2"></head><body bgcolor="white" text="black" link="#0000FF" vlink="#840084" alink="#0000FF"><div lang="en" class="book" title="Simulink Default Report"><div class="titlepage"><div><div><h1 class="title"><a name="d12e1"></a>Simulink Default Report</h1></div><div><h2 class="subtitle"></h2></div><div><div class="author"><h3 class="author"><span class="firstname">scorpii
</span></h3></div></div><div><p class="pubdate">28-Mar-2016 17:23:50</p></div></div><hr></div><div class="toc"><p><b>Table of Contents</b></p><dl><dt><span class="chapter"><a href="#35218bb1cf3c3a7b58d2eca93b736730">1. RocketFlight_TestModel</a></span></dt><dd><dl><dt><span class="sect1"><a href="#02cd22552f198fe19b15ad8d929388d6">RocketFlight_TestModel</a></span></dt></dl></dd></dl></div><div class="list-of-tables"><p><b>List of Tables</b></p><dl><dt>1.1. <a href="#d12e655">RocketFlight_TestModel<span> Simulation Parameters</span>
</a></dt><dt>1.2. <a href="#d12e750">Clock Block Properties</a></dt><dt>1.3. <a href="#d12e792">Demux Block Properties</a></dt><dt>1.4. <a href="#d12e855">RocketFlight_TestModel<span> System Information</span>
</a></dt><dt>1.5. <a href="#d12e921">Block Type Count</a></dt></dl></div><div class="chapter" title="Chapter 1. RocketFlight_TestModel"><div class="titlepage"><div><div><h2 class="title"><a name="35218bb1cf3c3a7b58d2eca93b736730"></a>Chapter 1. RocketFlight_TestModel</h2></div></div></div><div class="toc"><p><b>Table of Contents</b></p><dl><dt><span class="sect1"><a href="#02cd22552f198fe19b15ad8d929388d6">RocketFlight_TestModel</a></span></dt></dl></div><div class="itemizedlist"><ul class="itemizedlist" type="disc" compact><li class="listitem"><p class="simpara">
<a class="link" href="#35218bb1cf3c3a7b58d2eca93b736730" title="Chapter 1. RocketFlight_TestModel">RocketFlight_TestModel</a>
</p><div class="itemizedlist"><ul class="itemizedlist" type="circle" compact><li class="listitem"><p class="simpara">
Rocket 2DOF Kinematics Model
</p><div class="itemizedlist"><ul class="itemizedlist" type="square" compact><li class="listitem"><p class="simpara">
Atmospheric Model
</p><div class="itemizedlist"><ul class="itemizedlist" type="disc" compact><li class="listitem">
Atmospheric Sanity
</li><li class="listitem"><p class="simpara">
Rocket ISA Model
</p><div class="itemizedlist"><ul class="itemizedlist" type="circle" compact><li class="listitem">
ISA Model
</li></ul></div></li></ul></div></li><li class="listitem"><p class="simpara">
Critical Areas
</p><div class="itemizedlist"><ul class="itemizedlist" type="disc" compact><li class="listitem"><p class="simpara">
Frontal Reference Area
</p><div class="itemizedlist"><ul class="itemizedlist" type="circle" compact><li class="listitem">
AreaReferenceFrontal
</li></ul></div></li><li class="listitem"><p class="simpara">
Wetted Area of Body
</p><div class="itemizedlist"><ul class="itemizedlist" type="circle" compact><li class="listitem">
Wetted Body of Area
</li></ul></div></li></ul></div></li><li class="listitem"><p class="simpara">
Propulsion Dynamics
</p><div class="itemizedlist"><ul class="itemizedlist" type="disc" compact><li class="listitem"><p class="simpara">
Dynamic Motor Model
</p><div class="itemizedlist"><ul class="itemizedlist" type="circle" compact><li class="listitem">
Dynamic Sanity
</li><li class="listitem">
Thurst Curve Data
</li></ul></div></li><li class="listitem">
Propulsion Input Data
</li></ul></div></li><li class="listitem">
Reference Area at AOA
</li><li class="listitem"><p class="simpara">
Rocket 2DOF Translation
</p><div class="itemizedlist"><ul class="itemizedlist" type="disc" compact><li class="listitem"><p class="simpara">
Kinematic Model1
</p><div class="itemizedlist"><ul class="itemizedlist" type="circle" compact><li class="listitem">
Kinematic Sanity
</li><li class="listitem">
Rocket Vertical Flight Model
</li></ul></div></li><li class="listitem">
Rocket Drift
</li><li class="listitem"><p class="simpara">
Rocket Trajectory
</p><div class="itemizedlist"><ul class="itemizedlist" type="circle" compact><li class="listitem">
2D Vector
</li><li class="listitem">
Trajectory Angle
</li></ul></div></li></ul></div></li><li class="listitem"><p class="simpara">
Rocket Drag Model
</p><div class="itemizedlist"><ul class="itemizedlist" type="disc" compact><li class="listitem">
2D Vector
</li><li class="listitem"><p class="simpara">
Critical Areas
</p><div class="itemizedlist"><ul class="itemizedlist" type="circle" compact><li class="listitem"><p class="simpara">
Frontal Reference Area
</p><div class="itemizedlist"><ul class="itemizedlist" type="square" compact><li class="listitem">
AreaReferenceFrontal
</li></ul></div></li><li class="listitem"><p class="simpara">
Wetted Area of Body
</p><div class="itemizedlist"><ul class="itemizedlist" type="square" compact><li class="listitem">
Wetted Body of Area
</li></ul></div></li></ul></div></li><li class="listitem">
Drag Force
</li><li class="listitem">
Mach Number
</li><li class="listitem"><p class="simpara">
Reynolds Number
</p><div class="itemizedlist"><ul class="itemizedlist" type="circle" compact><li class="listitem">
Actual Reynolds Number
</li><li class="listitem">
Critical Reynolds Number
</li></ul></div></li><li class="listitem"><p class="simpara">
Rocket Drag Coefficient
</p><div class="itemizedlist"><ul class="itemizedlist" type="circle" compact><li class="listitem"><p class="simpara">
Base Drag Coefficient
</p><div class="itemizedlist"><ul class="itemizedlist" type="square" compact><li class="listitem">
Base Drag Coefficient
</li><li class="listitem">
Base Drag Coefficient (Normalized)
</li></ul></div></li><li class="listitem"><p class="simpara">
Fin Pressure Drag Coefficient
</p><div class="itemizedlist"><ul class="itemizedlist" type="square" compact><li class="listitem">
Normalized Fin Pressure Drag Coefficient
</li><li class="listitem">
Stagnation Pressure Coefficient
</li></ul></div></li><li class="listitem">
Nose Cone Drag Coefficient
</li><li class="listitem"><p class="simpara">
Parasitic Drag Coefficient
</p><div class="itemizedlist"><ul class="itemizedlist" type="square" compact><li class="listitem">
Parasitic Drag Coefficient
</li><li class="listitem">
Parasitic Drag Coefficient (Normalized)
</li><li class="listitem">
Stagnation Drag Coefficient
</li></ul></div></li><li class="listitem">
Rocket Drag at AOA
</li><li class="listitem"><p class="simpara">
Skin Friction Drag Coefficient
</p><div class="itemizedlist"><ul class="itemizedlist" type="square" compact><li class="listitem">
Skin Friction Drag Coefficient (normalized)
</li><li class="listitem">
Skin Friction Drag Coefficient (uncorrected for compressibility)
</li><li class="listitem">
Skin Friction Drag Coefficient (corrected for compressibility)
</li><li class="listitem">
Wetted Area of Fin
</li></ul></div></li></ul></div></li><li class="listitem">
Zero until leaving launch guide
</li></ul></div></li></ul></div></li><li class="listitem"><p class="simpara">
Shawn Angular Flight Model
</p><div class="itemizedlist"><ul class="itemizedlist" type="square" compact><li class="listitem"><p class="simpara">
Shawn Angular Model
</p><div class="itemizedlist"><ul class="itemizedlist" type="disc" compact><li class="listitem"><p class="simpara">
Angular Harmonic Motion
</p><div class="itemizedlist"><ul class="itemizedlist" type="circle" compact><li class="listitem"><p class="simpara">
Angular Frequency
</p><div class="itemizedlist"><ul class="itemizedlist" type="square" compact><li class="listitem">
Zero until leaving launch guide
</li></ul></div></li><li class="listitem">
Initial Amplitude
</li><li class="listitem">
Inverse Time Constant
</li><li class="listitem">
Natural Frequency
</li><li class="listitem">
Phase Angle
</li><li class="listitem">
Rocket Damping Ratio
</li><li class="listitem"><p class="simpara">
Rocket Angular Flight Model Simplified
</p><div class="itemizedlist"><ul class="itemizedlist" type="square" compact><li class="listitem">
If NaN then ZERO
</li></ul></div></li></ul></div></li><li class="listitem"><p class="simpara">
Barrowman Method
</p><div class="itemizedlist"><ul class="itemizedlist" type="circle" compact><li class="listitem"><p class="simpara">
Aerodynamic Damping Moment Coefficient
</p><div class="itemizedlist"><ul class="itemizedlist" type="square" compact><li class="listitem">
Body Lift Correction
</li><li class="listitem">
Finset
</li><li class="listitem">
Subsystem
</li><li class="listitem">
Subsystem1
</li><li class="listitem">
Zero until leaving launch guide
</li></ul></div></li><li class="listitem"><p class="simpara">
Center of Pressure
</p><div class="itemizedlist"><ul class="itemizedlist" type="square" compact><li class="listitem">
Body Tube Cone Center
</li><li class="listitem">
Fin Set Center
</li><li class="listitem">
Modified Center of Pressure
</li><li class="listitem">
Nose Cone Center
</li><li class="listitem">
Rocket Planform Center
</li></ul></div></li><li class="listitem">
Corrective Moment Coefficient
</li><li class="listitem">
Dynamic Center Of Gravity
</li><li class="listitem">
Dynamic Moment of Inertia
</li><li class="listitem">
Longitudinal Static Stability Margin
</li><li class="listitem">
Normal Force
</li><li class="listitem"><p class="simpara">
Propulsion Damping Moment
</p><div class="itemizedlist"><ul class="itemizedlist" type="square" compact><li class="listitem">
Zero until leaving launch guide
</li></ul></div></li><li class="listitem"><p class="simpara">
Rocket Body Lift Correction
</p><div class="itemizedlist"><ul class="itemizedlist" type="square" compact><li class="listitem">
Zero until leaving launch guide
</li></ul></div></li><li class="listitem">
Rocket Normal Force Coefficient
</li><li class="listitem"><p class="simpara">
Rocket Stability Derivative
</p><div class="itemizedlist"><ul class="itemizedlist" type="square" compact><li class="listitem">
Body Tube Stability Derivative
</li><li class="listitem"><p class="simpara">
Fin Set Stability Derivative
</p><div class="itemizedlist"><ul class="itemizedlist" type="disc" compact><li class="listitem">
Fin-Body Interference Coefficient
</li></ul></div></li><li class="listitem">
Nose Cone Stability Derivative
</li></ul></div></li></ul></div></li><li class="listitem"><p class="simpara">
Wind Disturbance
</p><div class="itemizedlist"><ul class="itemizedlist" type="circle" compact><li class="listitem">
Zero until leaving launch guide
</li></ul></div></li><li class="listitem">
Zero until leaving launch guide
</li><li class="listitem">
Zero until leaving launch guide1
</li></ul></div></li></ul></div></li></ul></div></li></ul></div><div class="table"><a name="d12e655"></a><p class="title"><b>Table 1.1. RocketFlight_TestModel<span> Simulation Parameters</span>
</b></p><div class="table-contents"><table summary="RocketFlight_TestModel Simulation Parameters
 " width="100%" style="border-collapse: collapse;border-top: 0.5pt solid ; border-bottom: 0.5pt solid ; border-left: 0.5pt solid ; border-right: 0.5pt solid ; "><colgroup><col width="60*" align="left"><col width="60*" align="left"><col width="60*" align="left"></colgroup><tbody><tr><td style="border-right: 0.5pt solid ; border-bottom: 0.5pt solid ; " align="left">
<span class="emphasis"><em>Solver</em></span>
<span> </span>ode4</td><td style="border-right: 0.5pt solid ; border-bottom: 0.5pt solid ; " align="left">
<span class="emphasis"><em>ZeroCross</em></span>
<span> </span>on</td><td style="border-bottom: 0.5pt solid ; " align="left">
<span class="emphasis"><em>StartTime</em></span>
<span> </span>0.0<span> </span>
<span class="emphasis"><em>StopTime</em></span>
<span> </span>simulation_duration</td></tr><tr><td style="border-right: 0.5pt solid ; border-bottom: 0.5pt solid ; " align="left">
<span class="emphasis"><em>RelTol</em></span>
<span> </span>1e-3</td><td style="border-right: 0.5pt solid ; border-bottom: 0.5pt solid ; " align="left">
<span class="emphasis"><em>AbsTol</em></span>
<span> </span>auto</td><td style="border-bottom: 0.5pt solid ; " align="left">
<span class="emphasis"><em>Refine</em></span>
<span> </span>1</td></tr><tr><td style="border-right: 0.5pt solid ; " align="left">
<span class="emphasis"><em>InitialStep</em></span>
<span> </span>auto</td><td style="border-right: 0.5pt solid ; " align="left">
<span class="emphasis"><em>FixedStep</em></span>
<span> </span>timestep</td><td style="" align="left">
<span class="emphasis"><em>MaxStep</em></span>
<span> </span>auto</td></tr></tbody></table></div></div><br class="table-break"><a name="d12e750"></a><div class="table"><p class="title"><b>Table 1.2. Clock Block Properties</b></p><div class="table-contents"><table summary="Clock Block Properties" border="1" cellspacing="0" fastRender="1" width="100%"><col width="60*"><col width="60*"><col width="60*"><col width="60*"><thead><tr>
<th align="left">Name</th>
<th align="left">Parent</th>
<th align="left">Display Time</th>
<th align="left">Decimation</th>
</tr></thead><tbody><tr>
<td align="left">
<a name="79c5b1168bece1cac2e5fb43f666f9a8"></a>Clock1</td>
<td align="left">
<a class="link" href="#35218bb1cf3c3a7b58d2eca93b736730" title="Chapter 1. RocketFlight_TestModel">RocketFlight_TestModel</a>
</td>
<td align="left">on</td>
<td align="left">10</td>
</tr></tbody></table></div></div><a name="d12e792"></a><div class="table"><p class="title"><b>Table 1.3. Demux Block Properties</b></p><div class="table-contents"><table summary="Demux Block Properties" border="1" cellspacing="0" fastRender="1" width="100%"><col width="60*"><col width="60*"><col width="60*"><col width="60*"><col width="60*"><thead><tr>
<th align="left">Name</th>
<th align="left">Parent</th>
<th align="left">Outputs</th>
<th align="left">Display Option</th>
<th align="left">Bus Selection Mode</th>
</tr></thead><tbody><tr>
<td align="left">
<a name="96ba28fe10e5fba51cb314122597d892"></a>Demux</td>
<td align="left">
<a class="link" href="#35218bb1cf3c3a7b58d2eca93b736730" title="Chapter 1. RocketFlight_TestModel">RocketFlight_TestModel</a>
</td>
<td align="left">2</td>
<td align="left">bar</td>
<td align="left">off</td>
</tr></tbody></table></div></div><div class="sect1" title="RocketFlight_TestModel"><div class="titlepage"><div><div><h2 class="title" style="clear: both"><a name="02cd22552f198fe19b15ad8d929388d6"></a>RocketFlight_TestModel</h2></div></div></div><div class="mediaobject"><map name="d12e847"><area coords="458,263,479,283" shape="rect" href="#79c5b1168bece1cac2e5fb43f666f9a8"><area coords="379,11,383,38" shape="rect" href="#96ba28fe10e5fba51cb314122597d892"></map><img src="./simulink-default_html_files/image-002-sl.png" usemap="%0A #d12e847" ismap="" border="0"></div><div class="table"><a name="d12e855"></a><p class="title"><b>Table 1.4. RocketFlight_TestModel<span> System Information</span>
</b></p><div class="table-contents"><table summary="RocketFlight_TestModel System Information
 " width="100%" style="border-collapse: collapse;border-top: 0.5pt solid ; border-bottom: 0.5pt solid ; border-left: 0.5pt solid ; border-right: 0.5pt solid ; "><colgroup><col width="3540*" align="left"><col width="8460*" align="left"></colgroup><tbody><tr><td style="border-right: 0.5pt solid ; border-bottom: 0.5pt solid ; " align="right">Name</td><td style="border-bottom: 0.5pt solid ; " align="left">RocketFlight_TestModel</td></tr><tr><td style="border-right: 0.5pt solid ; border-bottom: 0.5pt solid ; " align="right">Parent</td><td style="border-bottom: 0.5pt solid ; " align="left"><root></td></tr><tr><td style="border-right: 0.5pt solid ; border-bottom: 0.5pt solid ; " align="right">Description</td><td style="border-bottom: 0.5pt solid ; " align="left"> </td></tr><tr><td style="border-right: 0.5pt solid ; border-bottom: 0.5pt solid ; " align="right">Tag</td><td style="border-bottom: 0.5pt solid ; " align="left"> </td></tr><tr><td style="border-right: 0.5pt solid ; border-bottom: 0.5pt solid ; " align="right">Blocks</td><td style="border-bottom: 0.5pt solid ; " align="left">
<table border="0" summary="Simple list" class="simplelist"><tr><td>
Angular Motion Scope
</td></tr><tr><td>
<a class="link" href="#79c5b1168bece1cac2e5fb43f666f9a8">Clock1</a>
</td></tr><tr><td>
<a class="link" href="#96ba28fe10e5fba51cb314122597d892">Demux</a>
</td></tr><tr><td>
Rocket 2DOF Kinematics Model
</td></tr><tr><td>
Shawn Angular Flight Model
</td></tr></table>
</td></tr><tr><td style="border-right: 0.5pt solid ; " align="right">LinkStatus</td><td style="" align="left">N/A</td></tr></tbody></table></div></div><br class="table-break"><a name="d12e921"></a><div class="table"><p class="title"><b>Table 1.5. Block Type Count</b></p><div class="table-contents"><table summary="Block Type Count" border="1" cellspacing="0" fastRender="1" width="100%"><col width="120*"><col width="60*"><col width="240*"><thead><tr>
<th align="left">BlockType</th>
<th align="left">Count</th>
<th align="left">Block Names</th>
</tr></thead><tbody><tr>
<td align="left">SubSystem</td>
<td align="left">2</td>
<td align="left">
Rocket 2DOF Kinematics Model, Shawn Angular Flight Model
</td>
</tr><tr>
<td align="left">Demux</td>
<td align="left">1</td>
<td align="left">
<a class="link" href="#96ba28fe10e5fba51cb314122597d892">Demux</a>
</td>
</tr><tr>
<td align="left">Clock</td>
<td align="left">1</td>
<td align="left">
<a class="link" href="#79c5b1168bece1cac2e5fb43f666f9a8">Clock1</a>
</td>
</tr></tbody></table></div></div></div></div></div></body></html>